Low Energy Flight: Orbital Dynamics and Mission Trajectory Design / by Jianping Yuan, Yu Cheng, Jinglang Feng, Chong Sun

By:

Yuan, Jianping, 1957- [VerfasserIn]

Contributor(s):

Resource type: Ressourcentyp: Buch (Online)Book (Online)Language: English Series: Springer eBooks Engineering | Springer eBook CollectionPublisher: Singapore : Springer, 2019Description: 1 Online-Ressource (X, 209 p. 136 illus., 108 illus. in color)ISBN:

9789811361302

Subject(s):

Additional physical formats: 9789811361296 | Erscheint auch als: 978-981-13-6129-6 Druck-AusgabeDDC classification:

629.1 23

MSC: MSC: *70-02 | 70M20LOC classification:

TL787-4050.22

DOI: DOI: 10.1007/978-981-13-6130-2Online resources:

Summary: Introduction -- Continuous Low Thrust Trajectory Design and optimization -- Study of the Transfer Between Libration Point Orbits and Lunar Orbits in Earth-Moon System -- Lorentz Force Formation Flying in Earth-Moon System -- Orbital Dynamics in the Irregular Gravitational Field - Resonance -- Orbital Dynamics in the Vicinity of Contact Binary Asteroid Systems -- AppendicesSummary: The book focuses on the orbital dynamics and mission trajectory (transfer or target trajectory) design of low-energy flight in the context of modern astrodynamics. It investigates various topics that either offer new methods for solving classical problems or address emerging problems that have yet to be studied, including low-thrust transfer trajectory design using the virtual gravity field method; transfer in the three-body system using invariant manifolds; formation flying under space-borne artificial magnetic fields; and the orbital dynamics of highly irregular asteroids. It also features an extensive study of the orbital dynamics in the vicinity of contact binary asteroids, including the 1:1 ground-track resonance, the equilibrium points and their stability, and the third-order analytical solution of orbital motion in the vicinity of the non-collinear equilibrium point. Given its breadth of coverage, the book offers a valuable reference guide for all engineers and researchers interested in the potential applications of low-energy space missionsPPN: PPN: 1666748315Package identifier: Produktsigel: ZDB-2-ENG | ZDB-2-SEB | ZDB-2-SXE

Holdings ( 0 )

No physical items for this record